View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52586U 26145.37284410 +.00000000 +00000-0 +31109-4 0 00004
2 52586 53.2137 134.8755 0000948 73.0690 287.0406 15.08842750 05
| Epoch (UTC): | 25 May 2026 08:56:53 |
| Eccentricity: | 0.0000948 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 134.8755° |
| argument of perigee: | 73.0690° |
| revolutions per day: | 15.08842750 |
| mean anomaly at epoch: | 287.0406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|